About: Abe Mizet II

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The Abe Mizet II is a simple single seat ultralight of pusher configuration, built in Japan just after World War II. First flown in 1948, the sole example remained active twenty five years later.

Attributes	Values
rdf:type	Thing schema:Product mean of transportation Aircraft yago:Abstraction100002137 yago:Category105838765 yago:Cognition100023271 yago:Concept105835747 yago:Content105809192 yago:Idea105833840 yago:Kind105839024 yago:PsychologicalFeature100023100 aircraft yago:Type105840188
rdfs:label	Abe Mizet II (en)
rdfs:comment	The Abe Mizet II is a simple single seat ultralight of pusher configuration, built in Japan just after World War II. First flown in 1948, the sole example remained active twenty five years later. (en)
dct:subject	1940s Japanese civil aircraft
Wikipage page ID	37516428 (xsd:integer)
Wikipage revision ID	993125680 (xsd:integer)
Link from a Wikipage to another Wikipage	Ultralight Homebuilt Empennage Leading edge Trailing edge Pusher configuration Japan 1940s Japanese civil aircraft Chord (aircraft) World War II Rudder dbr:Paburica Ventral Tricycle undercarriage
Link from a Wikipage to an external page
sameAs	Abe Mizet II Abe Mizet II Abe Mizet II
span m	7.600000 (xsd:double)
wing area sqm	9 (xsd:integer)
wing loading kg/m	28.200000 (xsd:double)
dbp:wikiPageUsesTemplate	dbt:Reflist dbt:Aircontent dbt:Aircraft_specs dbt:Infobox_Aircraft_Type
dbp:primeUnits%3F_	met (en)
first flight	1948-12-09 (xsd:date)
national origin	Japan
crew	One (en)
designer	K. Abe (en)
ref	Jane's All the World's Aircraft 1974-75 (en)
type	Single seat homebuilt ultralight (en)
has abstract	The Abe Mizet II is a simple single seat ultralight of pusher configuration, built in Japan just after World War II. First flown in 1948, the sole example remained active twenty five years later. (en)
airfoil	Göttingen 387 (en)
aspect ratio	6.500000 (xsd:double)
empty weight kg	165 (xsd:integer)
eng1 hp	25 (xsd:integer)
eng1 name	dbr:Paburica
eng1 number	1 (xsd:integer)
eng1 type	800 (xsd:integer)
height m	2.200000 (xsd:double)
height note	over til (en)
length m	5.500000 (xsd:double)
max takeoff weight kg	255 (xsd:integer)
number built	1 (xsd:integer)
power/mass	73 (xsd:integer)
prop blade number	2 (xsd:integer)
prop dia m	1.100000 (xsd:double)
prop dia note	wooden pusher (en)
gold:hypernym	Ultralight
prov:wasDerivedFrom	wikipedia-en:Abe_Mizet_II?oldid=993125680&ns=0
page length (characters) of wiki page	5031 (xsd:nonNegativeInteger)
number built	1 (xsd:nonNegativeInteger)
origin	Japan
type	Homebuilt
foaf:isPrimaryTopicOf	wikipedia-en:Abe_Mizet_II
is Link from a Wikipage to another Wikipage of	List of aircraft (0–Ah)
is foaf:primaryTopic of	wikipedia-en:Abe_Mizet_II

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